FIELD: machine building.
SUBSTANCE: invention relates to the field of gas turbine engine (GTE) automatic control, namely, to the afterburner combustion chamber operation modes control systems. Invention differs from existing ones in that it additionally includes series-connected gas flow full pressure sensor installed at the output of afterburner combustion chamber, fuel manifold control valve position regulator mounted on the afterburner fuel distributor housing, the outlet of which is connected to the up-down fuel distributor second inlet.
EFFECT: technical result is improvement of efficiency of working process control in afterburner combustion chamber due to measurement of gas flow total pressure at output of afterburner combustion chamber and correction of fuel supply point ahead of flame stabilizer in afterburner combustion chamber.
1 cl, 3 dwg
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